کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1661643 | 1517695 | 2007 | 7 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی مواد
فناوری نانو (نانو تکنولوژی)
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils](/preview/png/1661643.png)
چکیده انگلیسی
Thermal barrier coatings (TBCs) must successfully resist damage from a variety of environmental and mechanical mechanisms to be viable on turbine airfoils. This paper reviews engine-operative TBC damage mechanisms and the requirements for life methods that enable a designer and engine operator to achieve acceptable TBCed component lives. Understanding TBC damage mechanisms facilitates development of advanced TBCs. The following damage mechanisms are discussed:
• growth and cracking of the bond coating's thermally grown oxide and its interfaces
• molten deposit (sulfate salt and calcia–magnesia–alumina–silicate) wicking into TBC
• sintering shrinkage, particle impact, bond coating creep
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Surface and Coatings Technology - Volume 202, Issues 4–7, 15 December 2007, Pages 658–664
Journal: Surface and Coatings Technology - Volume 202, Issues 4–7, 15 December 2007, Pages 658–664
نویسندگان
Tom Strangman, Derek Raybould, Ahsan Jameel, Wil Baker,